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Clarification and Application of Turbulent Mixing for Hydrogen Air Supersonic Mixing

Clarification and Application of Turbulent Mixing for Hydrogen Air Supersonic Mixing
氢气-空气超音速混合湍流混合的澄清及应用
批准号:
17560694
负责人:
ARAI Takakage
金额:
$2.24万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for Scientific Research (C)
财政年份:
2005
资助国家:
日本
项目状态:
已结题
起止时间:
2005 至 2006

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中文摘要
翻译
本研究分为混合评价和混合增强两部分。首先,通过铂丝催化反应验证了超声速混合条件时间序列评价的有效性。气体氢从喷射器注入超音速自由流(马赫数1.81)。采用带铂丝和参考丝(镍丝)的w型探头,对超声速混合时间序列条件进行了评价。在保持导线温度不变的情况下,通过同时测量各电路所提供的每一功率来进行评价。具体提供给铂丝的电力取决于催化热释放率(给予氢浓度)和流动对流。同时,对镍丝的影响取决于流动对流。结果表明,随着混合的发展,这些电功率之间的相关系数增大。同时还对氦、空气和无二次注入的情况进行了调查,并与氢气注入的情况进行了比较。结果表明,利用该评价方法可以测量空气-氢超声速混合层或湍流相干运动的时间序列行为。其次,对于超声速混合增强,实验表明大尺度的流向涡旋似乎是最有利的,如质量通量波动的FFT频谱分析显示,功率谱部分遵循Kolmogorov -5/3幂律,表明流向涡旋的击穿产生了高混合功率的小尺度湍流涡旋。本文采用PIV、纹影显示、热线风速仪和CFD等方法研究了湍流涡旋的击穿过程。实验结果表明,在涡旋雷诺数ReΓ=Γ/v=1.3×10^4及以上时,流向涡旋击穿成小尺度湍流,且流向涡旋上的横向结构参与了其击穿过程。从计算分析来看,坡道上剪切层的振荡会使流向涡不稳定并导致其破裂。少
英文摘要
This research has two parts of the mixing evaluation and mixing enhancement.First, an experimental study was carried out to confirm the validity of time series evaluation of supersonic mixing condition by using catalytic reaction on a platinum wire. Gaseous hydrogen was injected into supersonic free-stream (Mach 1.81) from injector. Time series condition of supersonic mixing was evaluated by using W-type probe which has a platinum wire and reference wire (nickel wire). The evaluation was done by simultaneously measuring each electric power supplied by each electric circuit which kept the temperature of wire constant. Specifically supplied electric power to Pt wire depended on catalytic heat release rate (giving hydrogen concentration) and flow convection. Meanwhile that to Ni wire depended on flow convection. The result showed that correlation coefficient between these electric powers increased when mixing developed. Investigations were also conducted for helium, air and no secondary i … More njectant cases to compare with the hydrogen injectant case. The results indicated that it was possible to measure the time-series behavior of air-hydrogen supersonic mixing layer or coherent motion of turbulence by using this evaluation.Second, for supersonic mixing enhancement, experiments suggested that large scale streamwise vortices seemed to be the most advantageous, for example, FFT spectrum analysis of mass flux fluctuations showed that the power spectrum partly follows Kolmogorov's -5/3 power law, indicating that the breakdown of streamwise vortices occurred to generate small scale turbulent eddies of high mixing power. The present study examined the breakdown process of streamwise vortices by using PIV, schlieren visualization, hot-wire anemometer and CFD. The experimental results showed that the breakdown of streamwise vortices into small scale turbulence occured at the vortex Reynolds number ReΓ=Γ/v=1.3×10^4 or more, and that the lateral structure on streamewise vortices took a part in its breakdown process. From the computational analysis, the oscillation of shear layer from ramp could make the streamwise vortices unstable and cause its breakdown. Less
期刊论文(29)
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会议论文
触媒反応を利用した糠-空気超音速混合の評価
利用催化反应评价麸皮-空气超声混合
DOI: --
发表时间: 2007
期刊: JAXA SP 宇宙航空研究開発機構特別資料「境界層遷移の解明と制御」研究会講演論文集(第37回,第38回) JAXA-SP-06-013
影响因子: --
作者: [A.KONDO, 新井隆景]
通讯作者: 新井隆景
強い主流流れが励起する境界層撹乱の代数的増幅
强主流流激发边界层扰动的代数放大
DOI: --
发表时间: 2005
期刊: 日本流体力学会年会2005講演論文集 24巻別冊
影响因子: --
作者: [S.SAKAUE, N.NINAMI, M.NISHIOKA, S.Sakaue, 近藤暁, 坂上昇史, T.ARAI, 新井隆景, 黒川幸二]
通讯作者: 黒川幸二
Evaluation of Hydrogen-Air Supersonic Mixing Condition using Catalytic reaction
利用催化反应评价氢气-空气超音速混合条件
DOI: --
发表时间:
期刊: Proceedings of the 37^<th> and 38^<th> JAXA Workshops on "Investigation and Control of Boundary-layer transition"
影响因子: --
作者: [T.MORISAKI, S.SAKAUE, M.NISHIOKA, T.ARM, 新井隆景, 黒川幸二, 坂上昇史, T.ARAI]
通讯作者: T.ARAI
縦渦の導入された超音速乱流混合場のPIV計測
引入纵向涡的超音速湍流混合场PIV测量
DOI: --
发表时间: 2006
期刊: 日本流体力学学会誌「ながれ」 25巻別冊
影响因子: --
作者: [A.KONDO, S.SAKAUE, T.ARAI, 新井隆景, S.Sakaue, T.Arai, 近藤暁]
通讯作者: 近藤暁
共 20 条
    Supersonic Streamwise Vortices Breakdown and Its Application for Supersonic Mixing
    • 批准号:
      20560739
    • 项目类别:
      Grant-in-Aid for Scientific Research (C)
    • 资助金额:
      $2.91万
    • 财政年份:
      2008
    • 负责人:
      ARAI Takakage
    • 依托单位:
    Shock Induced Combustion and Flame Folding in Supersonic Combustion Ramjet Engine
    • 批准号:
      13650960
    • 项目类别:
      Grant-in-Aid for Scientific Research (C)
    • 资助金额:
      $2.24万
    • 财政年份:
      2001
    • 负责人:
      ARAI Takakage
    • 依托单位:
    SUPERSONIC MIXING AND COMBUSTION OF HYDROGEN USING HIGH-ENTHALPY SHOCK TUNNEL
    • 批准号:
      11650938
    • 项目类别:
      Grant-in-Aid for Scientific Research (C)
    • 资助金额:
      $2.3万
    • 财政年份:
      1999
    • 负责人:
      ARAI Takakage
    • 依托单位:
    海外基金